NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Preliminary Design Of Adhesively Bonded Composite JointsJoints symmetrical and long enough to withstand cyclic loads and hygrothermal effects. Step-by-step procedure for preliminary design of adhesively bonded joints between laminated fiber-reinforced-matrix composite bars based on simplified methods for prediction of microstresses and local strengths, including interlaminar strengths. Involves approximate calculations of stresses in various components of joint. Includes calculations to determine such critical parameters as minimum length, maximum shear stress in adhesive, and peeloff stress. Deleterious effects of cyclic loading, increased temperature, and humidity also taken into account.
Document ID
19920000616
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Chamis, C. C.
(NASA Lewis Research Center, Cleveland, OH.)
Murthy, P. L. N.
(NASA Lewis Research Center, Cleveland, OH.)
Date Acquired
August 15, 2013
Publication Date
October 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 10
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-15050
Accession Number
92B10616
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available